Abstract
Composite materials are known to have starkly non-linear dynamic behaviour. As such, when considering the use of composite materials in dynamic environments, it is important to understand the variations in non-linear behaviour that can occur as a result of fatigue damage. This work has gathered data for numerous components which are trialled under High Cycle Fatigue (HCF) conditions with regular stepped sine investigations of resonant response at two or more modes. The resultant non-linear behaviour across the endurance test is compared and features are investigated. Non-linear responses for two differing specimen damage scenarios are investigated; artificial delamination at the mid-plane and delamination occurrence from terminated plies. Correlations between non-linear behaviour at different modes are observed and changes due to the increasing presence of damage are investigated.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Salpekar SA, Raju IS, O’Brien TK (1991) Strain-energy-release rate analysis of delamination in a tapered laminate subjected to tension load. J Compos Mater 25(2):118–141
Giannis S, Jeenjitkaew C (2011) Fatigue performance of tapered laminates with internal ply drop-offs: experiments and numerical predictions. 26th Annual technical conference of the American Society for Composites 2011and the 2nd Joint US-Canada conference on composites
Rami H, Wang SS (1990) Nonlinear behavior of fiber composite materials and its effect on the postbuckling response of laminated plates. National Center for Composite Materials Research at University of Illinois, Urbana
Singh G, Kanaka-Raju K, Venkateswara-Rao G, Iyengar NGR (1990) Non-linear vibrations of simply supported rectangular cross-ply plates. J Sound Vib 142(2):213–226
Ramesh C, Raju BB (1975) Large amplitude flexural vibration of cross ply laminated composite plates. Fibre Sci Technol 8(4):243–263
Han W, Petyt M (1997) Geometrically nonlinear vibration analysis of thin, rectangular plates using the hierarchical finite element method. II. 1st mode of laminated plates and higher modes of isotropic and laminated plates. Comput Struct 63(2):309–318
Houmat A (2012) Nonlinear free vibration of a composite rectangular specially-orthotropic plate with variable fiber spacing. Compos Struct 94(10):3029–3036
Nayfeh AH, Mook DT (1995) Nonlinear oscillations. Wiley VCH, New York
Ueda Y (1979) Randomly transitional phenomena in the system governed by Duffing’s equation. J Stat Phys 20(2):181–196
Kovacic I, Rega G, Zukovic M (2012) On the influence of a constant force on the appearance of period-doubling bifurcations and chaos in a harmonically excited pure cubic oscillator. Chaos Soliton Fract 45(12):1531–1540
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2014 The Society for Experimental Mechanics, Inc.
About this paper
Cite this paper
Pickard, A.M.J. (2014). Composite Non-Linearity in High Cycle Fatigue Experimentation. In: Kerschen, G. (eds) Nonlinear Dynamics, Volume 2. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-319-04522-1_17
Download citation
DOI: https://doi.org/10.1007/978-3-319-04522-1_17
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-04521-4
Online ISBN: 978-3-319-04522-1
eBook Packages: EngineeringEngineering (R0)